最后介绍了近无激波机翼修型的工程设计方法。
Finally, an engineering approach for nearly shock-free wing design is introduced.
本文采用全位势方程，在超音速区采用虚拟气体假设，给出了跨音速无激波翼型设计的一种方法。
In this paper, a method for the transonic shock-free airfoil design, based on the full potential equation, using "fictitious gas" assumption, is presented.
本文介绍了可移动式无膜激波管工作原理和在这种新实验设备上进行光学测量的理论依据和实验结果。
In this paper, a set of experiments have been conducted in a movable diaphragmless shock tube, and some experimental data have been obtained.
无网格的MUSCL格式，这种方式能够较好的模拟激波问题，并且易于推广到高维。
Meshless MUSCL scheme, which resolves shock tube problems well and is easy to extend to higher dimensions.
无碰撞激波是空间等离子体和宇宙等离子体中的重要物理现象。
Collisionless shocks are the important physical phenomena in the space and cosmical plasmas.
在无耗散介质的定常、平面激波两边产生了小扰动。
Small disturbances are introduced on both sides of a steady, non-dissipative, plane shock wave.
我们按如下步骤研究了含激波的黑洞吸积流的线性稳定性问题：首先，我们研究无粘滞的等温吸积流。
We investigate the linear stability of a shocked accretion flow onto a black hole with the following procedures: First, we study the stability in the inviscid isothermal limit.
对粘性与无粘结果的比较显示，由泄漏流所产生的激波后阻塞区是由激波-漏流干扰所致，粘性的作用将削弱其面积和强度。
The comparison between the viscous and non-viscous simulations shows that the intensive blockage area is caused by shock-leakage flow interaction.
对粘性与无粘结果的比较显示，由泄漏流所产生的激波后阻塞区是由激波-漏流干扰所致，粘性的作用将削弱其面积和强度。
The comparison between the viscous and non-viscous simulations shows that the intensive blockage area is caused by shock-leakage flow interaction.
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